EP2394836B1 - Fuel tank - Google Patents
Fuel tank Download PDFInfo
- Publication number
- EP2394836B1 EP2394836B1 EP10738497.6A EP10738497A EP2394836B1 EP 2394836 B1 EP2394836 B1 EP 2394836B1 EP 10738497 A EP10738497 A EP 10738497A EP 2394836 B1 EP2394836 B1 EP 2394836B1
- Authority
- EP
- European Patent Office
- Prior art keywords
- fuel
- opening
- fuel tank
- siphon tube
- lid
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Not-in-force
Links
- 239000002828 fuel tank Substances 0.000 title claims description 74
- 239000000446 fuel Substances 0.000 claims description 173
- 239000007788 liquid Substances 0.000 claims description 18
- 238000005086 pumping Methods 0.000 description 4
- 230000000694 effects Effects 0.000 description 3
- 238000007789 sealing Methods 0.000 description 3
- 238000002485 combustion reaction Methods 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 230000001105 regulatory effect Effects 0.000 description 1
Images
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
- F02M37/00—Apparatus or systems for feeding liquid fuel from storage containers to carburettors or fuel-injection apparatus; Arrangements for purifying liquid fuel specially adapted for, or arranged on, internal-combustion engines
- F02M37/0076—Details of the fuel feeding system related to the fuel tank
- F02M37/0088—Multiple separate fuel tanks or tanks being at least partially partitioned
- F02M37/0094—Saddle tanks; Tanks having partition walls
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60K—ARRANGEMENT OR MOUNTING OF PROPULSION UNITS OR OF TRANSMISSIONS IN VEHICLES; ARRANGEMENT OR MOUNTING OF PLURAL DIVERSE PRIME-MOVERS IN VEHICLES; AUXILIARY DRIVES FOR VEHICLES; INSTRUMENTATION OR DASHBOARDS FOR VEHICLES; ARRANGEMENTS IN CONNECTION WITH COOLING, AIR INTAKE, GAS EXHAUST OR FUEL SUPPLY OF PROPULSION UNITS IN VEHICLES
- B60K15/00—Arrangement in connection with fuel supply of combustion engines or other fuel consuming energy converters, e.g. fuel cells; Mounting or construction of fuel tanks
- B60K15/03—Fuel tanks
- B60K15/077—Fuel tanks with means modifying or controlling distribution or motion of fuel, e.g. to prevent noise, surge, splash or fuel starvation
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
- F02M37/00—Apparatus or systems for feeding liquid fuel from storage containers to carburettors or fuel-injection apparatus; Arrangements for purifying liquid fuel specially adapted for, or arranged on, internal-combustion engines
- F02M37/0011—Constructional details; Manufacturing or assembly of elements of fuel systems; Materials therefor
- F02M37/0023—Valves in the fuel supply and return system
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
- F02M37/00—Apparatus or systems for feeding liquid fuel from storage containers to carburettors or fuel-injection apparatus; Arrangements for purifying liquid fuel specially adapted for, or arranged on, internal-combustion engines
- F02M37/02—Feeding by means of suction apparatus, e.g. by air flow through carburettors
- F02M37/025—Feeding by means of a liquid fuel-driven jet pump
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
- F02M37/00—Apparatus or systems for feeding liquid fuel from storage containers to carburettors or fuel-injection apparatus; Arrangements for purifying liquid fuel specially adapted for, or arranged on, internal-combustion engines
- F02M37/04—Feeding by means of driven pumps
- F02M37/08—Feeding by means of driven pumps electrically driven
- F02M37/10—Feeding by means of driven pumps electrically driven submerged in fuel, e.g. in reservoir
- F02M37/103—Mounting pumps on fuel tanks
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
- F02M37/00—Apparatus or systems for feeding liquid fuel from storage containers to carburettors or fuel-injection apparatus; Arrangements for purifying liquid fuel specially adapted for, or arranged on, internal-combustion engines
- F02M37/04—Feeding by means of driven pumps
- F02M37/08—Feeding by means of driven pumps electrically driven
- F02M37/10—Feeding by means of driven pumps electrically driven submerged in fuel, e.g. in reservoir
- F02M37/106—Feeding by means of driven pumps electrically driven submerged in fuel, e.g. in reservoir the pump being installed in a sub-tank
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T137/00—Fluid handling
- Y10T137/2713—Siphons
- Y10T137/2842—With flow starting, stopping or maintaining means
- Y10T137/2849—Siphon venting or breaking
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T137/00—Fluid handling
- Y10T137/7287—Liquid level responsive or maintaining systems
- Y10T137/7358—By float controlled valve
- Y10T137/7439—Float arm operated valve
- Y10T137/7485—Pivoted valve
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T137/00—Fluid handling
- Y10T137/8593—Systems
- Y10T137/85978—With pump
- Y10T137/86075—And jet-aspiration type pump
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T137/00—Fluid handling
- Y10T137/8593—Systems
- Y10T137/86187—Plural tanks or compartments connected for serial flow
Definitions
- the present invention relates to a fuel tank including a first reservoir for reserving fuel, a second reservoir for reserving the fuel, and a siphon tube which extends between the first reservoir and the second reservoir and which is evacuated by a negative pressure generator.
- Fuel tanks are used to supply fuel to internal combustion engines.
- 4WD (four-wheel-drive) vehicles and FR (front engine, rear wheel drive) vehicles use a so-called saddle fuel tank, the bottom of which is upwardly recessed at the center portion in the width direction of the vehicle, in order for the fuel tank to avoid physical interference with the propeller shaft, which extends down the middle of the vehicle.
- the saddle fuel tank is generally divided into a first reservoir for reserving fuel and a second reservoir for reserving the fuel, and each of the first reservoir and the second reservoir is equipped with one fuel pumping system. Accordingly, the saddle fuel tank requires the two fuel pumping systems in comparison with fuel tanks for use in 2WD (two-wheel-drive) vehicles, and thus it is more costly and larger.
- JP 63 104671 U discloses a fuel tank including a first reservoir for storing fuel; a second reservoir for storing the fuel; and a siphon tube which extends between the first reservoir and the second reservoir and which is evacuated by a negative pressure generator; the fuel tank comprising a fuel introducing member connected to at least one open end of the siphon tube, wherein the fuel introducing member includes an opening for introducing the fuel therethrough; and a lid for closing the opening under its own weight of the lid when the liquid level of fuel has fallen just above the opening and the opening is disposed above the at least one open end of the siphon tube.
- DE 199 00 378 A1 discloses a saddle tank with a siphon tube connected to fuel introducing members equipped with a lid which opens and closes an inlet opening in dependence of a fuel level.
- JP 64 028318 U discloses a fuel introducing member with an inlet opening oriented in an upward direction, closed by a lid moving in a downward direction.
- the fuel tank level equalizer system includes a fuel tank 1 having two separate sections 1a, 1b, and operates to equalize fuel levels in the separate sections 1a, 1b through a siphon 2.
- the separate section 1b houses therein a fuel pump module 3 which has an outlet connected to a bypass pressure regulator 4.
- the regulator 4 has an outlet connected to a conduit 5 through which a liquid fuel is supplied to a nozzle 6a of a jet pump 6.
- the jet pump 6 is operated by the liquid fuel that is supplied to the nozzle 6a, drawing the fuel from fuel pickups 2a, 2b of the siphon 2 through the siphon 2.
- the fuel levels in the separate sections 1a, 1b are thus equalized through the siphon 2, and a single fuel level sensor 7 can monitor all the fuel levels in the vehicle.
- each of the fuel pickups 2a, 2b includes a flow valve assembly, not shown, which is actuated by a filter and a diaphragm.
- the filter is made of a flexible material having small openings, and the filter, when wetted, prevents air from flowing therethrough due to the capillary action of the liquid fuel. When there is no liquid fuel in the inlets of the fuel pickups, air is prevented from flowing therethrough by a liquid capillary seal of the filter.
- the fuel tank level equalizer system according to the conventional art is made up of a number of components and is complex in structure because the system includes actuating parts such as the filter having the small openings, the diaphragm, etc., and also includes the flow valve assembly. Therefore, the fuel tank level equalizer system according to the conventional art is costly to manufacture, and is low in productivity and endurance reliability. Furthermore, the fuel undergoes a large pressure loss because it flows through the filter having the small openings, resulting in a reduced siphon transfer speed. Accordingly, the filter tends to be clogged with dirt and also tend to be damaged.
- the filter fails to provide a sealing function when it is dry, not wet. When the filter is dry, it does not prevent air from flowing therethrough, and thus the filter does not provide a stable siphon effect. For example, if the fuel is present in only the separate section 1a, then no siphon effect is provided, and the fuel levels in the separate sections 1a, 1b can not be equalized.
- the present invention has been made in an effort to solve the above problems. It is an object of the present invention to provide a fuel tank which is capable of providing a desired siphon effect and using fuel in the fuel tank efficiently with a simple and economic structure.
- the fuel tank includes a first reservoir for storing fuel, a second reservoir for storing the fuel, and a siphon tube which extends between the first reservoir and the second reservoir and which is evacuated by a negative pressure generator.
- the fuel tank comprises a fuel introducing member connected to at least one open end of the siphon tube, wherein the fuel introducing member includes an opening for introducing the fuel therethrough, and a lid for closing the opening under its own weight of the lid when the opening is positioned above the liquid level of the fuel, and the opening is disposed below the at least one open end of the siphon tube.
- the fuel introducing member which is connected to at least one open end of the siphon tube, includes the opening for introducing the fuel in the fuel tank therethrough, and the opening is disposed below the upper end of the inner diameter of the one open end of the siphon tube. Therefore, the fuel can effectively be siphoned until the fuel level becomes lower than the upper end of the inner diameter of the at least one open end of the siphon tube.
- the fuel in the fuel tank can thus be used efficiently with a simple and economical structure.
- a fuel tank 10 according to a first embodiment of the present invention comprises a saddle fuel tank, and is mounted on a vehicle, not shown.
- the fuel tank 10 includes an upwardly curved saddle 14 on its bottom substantially centrally in the width direction (indicated by the arrow A) of the vehicle.
- the saddle 14 defines a main tank (first reservoir) 16 and a sub-tank (second reservoir) 18 in the fuel tank 10.
- a fuel pump module 20 is disposed in the main tank 16.
- the fuel pump module 20 comprises a fuel pump 22 including a pumping jet pump 24 which has a fuel inlet port 24a that is open toward the bottom of an inner surface 16a of the main tank 16 and also including a pressure regulator 26 connected to an outlet of the fuel pump 22.
- the pressure regulator 26 supplies a fuel F to an engine, not shown, through a fuel pipe 28, and has a suction branch pipe 30 extending therefrom.
- the branch pipe 30 has a distal end (lower end) connected to a suction jet pump 32 as a negative pressure generator.
- the fuel tank 10 houses therein a siphon tube 34 extending over the bottoms of inner surfaces 16a, 18a of the main tank 16 and the sub-tank 18.
- the siphon tube 34 includes a three-way joint 36 in its upper portion which includes a suction connector 36a having a check valve 38 disposed therein.
- the suction connector 36a is connected to an end of a suction tube 40, which has the other end connected to a suction side (negative pressure side) of the suction jet pump 32.
- the siphon tube 34 has an open end 34a disposed in the main tank 16 and directed in a width direction of the vehicle incorporating the fuel tank 10.
- a fuel introducing member 42a is connected to the open end 34a.
- the fuel introducing member 42a is of a hollow three-dimensional shape, e.g., a hollow rectangular parallelepiped, which is short in height directions, i.e., in the directions indicated by the arrow B.
- the fuel introducing member 42a basically comprises a base 44 in the form of a square tray and a substantially rectangular cover 46 mounted on the base 44.
- the cover 46 includes a joint 48 which is formed integrally with the cover 46. To the joint 48, the open end 34a of the siphon tube 34 is connected.
- the cover 46 has a circular opening 50 defined in an upper surface 46a thereof which is disposed below the upper end of an inner diameter of the open end 34a of the siphon tube 34 (see FIG. 3 ).
- the opening 50 which serves to introduce the fuel F from the main tank 16, is selectively opened and closed by a lid 52.
- the lid 52 is vertically openably and closably supported on the upper surface 46a of the cover 46 by a pivot shaft 54. If necessary, a float (floating member) 55 may be mounted on the lid 52.
- a float (floating member) 55 may be mounted on the lid 52.
- the float 55 may be dispensed with.
- the lid 52 has a stopper 53 formed integrally therewith for regulating an open position (angular position for its swinging movement) of the lid 52.
- the upper surface 46a of the cover 46 has a groove 56 defined therein around the opening 50.
- the base 44 and the cover 46 define a fuel channel 58 therebetween which connects the opening 50 and the open end 34a of the siphon tube 34 to each other.
- the fuel channel 58 has an opening area which is equal to or greater than the opening area of the opening 50.
- the opening area of the opening 50 and the opening area of the fuel channel 58 are equal to or greater than the opening area of the open end 34a of the siphon tube 34.
- the siphon tube 34 has an open end 34b disposed in the sub-tank 18.
- a fuel introducing member 42b is connected to the open end 34b.
- the fuel introducing member 42b is identical in structure to the fuel introducing member 42a. Those parts of the fuel introducing member 42b which are identical to those of the fuel introducing member 42a are denoted by identical reference characters, and will not be described below (see FIGS. 2 through 4 ). At least one of the fuel introducing members 42a, 42b may be employed.
- the fuel pump module 20 includes a float 60 for detecting the position of the liquid level Fs of the fuel F stored in the main tank 16.
- the fuel pump 22 of the fuel pump module 20 When the fuel pump 22 of the fuel pump module 20 is actuated, the fuel F stored in the main tank 16 is drawn from the fuel inlet port 24a by the pumping jet pump 24.
- the fuel F is supplied from the pressure regulator 26 through the fuel pipe 28 to the engine, and is also supplied through the branch pipe 30 to the suction jet pump 32, developing a negative pressure in the suction tube 40. Since the suction tube 40 is connected to the siphon tube 34 through the three-way joint 36, the siphon tube 34 is evacuated.
- the siphon tube 34 has its open end 34a placed in the fuel F stored in the main tank 16 and its other open end 34b placed in the sub-tank 18 which is initially free of the fuel F, with the lid 52 of the fuel introducing member 42b being closed (see FIG. 5 ).
- the lid 52 of the fuel introducing member 42b is opened.
- the fuel F now flows from the main tank 16 into the sub-tank 18 due to the siphoning function of the siphon tube 34. Therefore, the liquid level Fs of the fuel F in the main tank 16 and the liquid level Fs of the fuel F in the sub-tank 18 are brought into the same height.
- the fuel introducing member 42a which is connected to the open end 34a of the siphon tube 34 is mounted on the bottom of the main tank 16, and has its opening 50 disposed below the upper end of the inner diameter of the open end 34a (see FIG. 3 ).
- the fuel F in the main tank 16 can thus be used efficiently with a simple and economical structure.
- the fuel introducing member 42a which is mounted on the bottom of the main tank 16, is capable of effectively siphoning the fuel F stored in the main tank 16 without leaving a large quantity of fuel.
- the fuel introducing member 42a is disposed in the main tank 16, and the fuel introducing member 42b is disposed in the sub-tank 18. Therefore, any remaining fuel F can efficiently be siphoned from both the main tank 16 and the sub-tank 18.
- each of the fuel introducing members 42a, 42b is of a cubic or rectangular parallelepiped shape (hollow three-dimensional shape), which is short in a height direction, and has the opening 50 defined in the upper surface 46a and the lid 52 for opening and closing the opening 50. Even in a case where the vehicle is tilted on a slope or the like, its own weight of the lid 52 prevents the lid 52 from swinging in a direction to open the opening 50. In addition, in the fuel introducing members 42a, 42b, since the lid 52 closes the opening 50, the opening area of the opening 50 can be set to a large size, thereby for protection of the opening 50 against clogging or the like.
- the groove 56 is defined in the upper surface 46a around the opening 50.
- the opening area of the fuel channel 58 is equal to or greater than the opening area of the opening 50. Therefore, no flow resistance is present on the passage from the opening 50 to the fuel channel 58, and thus the fuel F in the main tank 16 and the sub-tank 18 can smoothly flow from the opening 50 to the fuel channel 58.
- the opening area of the opening 50 and the opening area of the fuel channel 58 are equal to or greater than the opening area of the open ends 34a, 34b of the siphon tube 34. Consequently, the fuel F can smoothly and reliably flow through the opening 50 and the fuel channel 58 into the siphon tube 34.
- FIG. 6 is a perspective view of each of fuel introducing members 70a, 70b of a fuel tank according to a second embodiment of the present invention.
- the upper surface 46a of the cover 46 of each of the fuel introducing members 70a, 70b has a first region 72 including the opening 50 and a second region 74 excluding the opening 50.
- the first region 72 is at a level lower than the second region 74.
- the remaining quantity of the fuel F is reduced and the lid 52 closes the opening 50 under its own weight, since the first region 72 including the opening 50 is at a level lower than the second region 74, the fuel F tends to remain in the first region 72. Therefore, when the lid 52 closes the opening 50, the remaining fuel F performs a sealing function to cause the lid 52 to close the opening 50 reliably.
- FIG. 7 is a perspective view of each of fuel introducing members 80a, 80b of a fuel tank according to a third embodiment of the present invention.
- FIG. 8 is a front elevational view of each of the fuel introducing members 80a, 80b.
- Each of the fuel introducing members 80a, 80b has recesses 82 defined at both sides of the lid 52, and a float (floating member) 84 is mounted on the lid 52.
- the float 84 includes projections 86 projecting downwardly into the respective recesses 82.
- the projections 86 have respective lower end faces 86a which are at a level lower than the opening 50 (see FIG. 8 ).
- the lower end faces 86a which are positioned at the lower end of the float 84 are at a level lower than the opening 50. Therefore, even in a case where the liquid level Fs of the fuel F is at a considerably low level, the float 84 exerts buoyant force thereby to open the opening 50.
- FIG. 9 is a sectional side elevational view of each of fuel introducing members 90a, 90b of a fuel tank according to a fourth embodiment of the present invention.
- Each of the fuel introducing members 90a, 90b includes a float (floating member) 94 mounted on the lid 52 by a joint member 92.
- the float 94 has a lower end positioned below the opening 50.
- the position where the lid 52 is opened by the float 94 can be set as low as possible. Therefore, the fourth embodiment offers the same advantages as with the third embodiment, e.g., the fourth embodiment is efficient in that the remaining amount of the fuel F can be suitably reduced.
- FIG. 10 is a perspective view of each of fuel introducing members 100a, 100b of a fuel tank according to a fifth embodiment of the present invention.
- Each of the fuel introducing members 100a, 100b is of an inverted trapezoidal shape (hollow three-dimensional shape) as viewed in front elevation with a narrower lower end, and includes an opening 50 defined in an upper surface thereof and a lid 52 for opening and closing the opening 50.
- FIG. 11 is a perspective view of each of fuel introducing members 110a, 110b of a fuel tank according to a sixth embodiment of the present invention.
- Each of the fuel introducing members 110a, 110b is of a hexagonal shape (hollow three-dimensional shape) as viewed in front elevation with widthwise opposite sides projecting outwardly in a dogleg shape, and includes an opening 50 defined in an upper surface thereof and a lid 52 for opening and closing the opening 50.
- FIG. 12 is a perspective view of each of fuel introducing members 120a, 120b of a fuel tank according to a seventh embodiment of the present invention.
- Each of the fuel introducing members 120a, 120b is of a trapezoidal shape (hollow three-dimensional shape) as viewed in front elevation with a wider lower end, and includes an opening 50 defined in an upper surface thereof and a lid 52 for opening and closing the opening 50.
- FIG. 13 is a perspective view of each of fuel introducing members 130a, 130b of a fuel tank according to an eighth embodiment of the present invention.
- Each of the fuel introducing members 130a, 130b is of an elliptical shape (hollow three-dimensional shape) as viewed in front elevation which is elongate transversely, and has an opening 50 defined in a curved upper surface 132 thereof and a lid 134 for opening and closing the opening 50.
- the lid 134 has a curved surface which corresponds to the curved upper surface 132.
- each of the fuel introducing members 130a, 130b may have a flat upper surface instead of the curved upper surface 132, and also have an opening 50 defined in the flat upper surface thereof and a lid 52 for opening and closing the opening 50. This holds true for ninth and subsequent embodiments to be described below.
- FIG. 14 is a perspective view of each of fuel introducing members 140a, 140b of a fuel tank according to a ninth embodiment of the present invention.
- Each of the fuel introducing members 140a, 140b is of an upper semicircular shape (hollow three-dimensional shape) as viewed in front elevation with a flat bottom surface 142, and has an opening 50 defined in a curved upper surface 144 thereof and a lid 146 for opening and closing the opening 50.
- the lid 146 has a curved surface which corresponds to the curved upper surface 144.
- FIG. 15 is a perspective view of each of fuel introducing members 150a, 150b of a fuel tank according to a tenth embodiment of the present invention.
- Each of the fuel introducing members 150a, 150b is of a lower semicircular shape (hollow three-dimensional shape) as viewed in front elevation with a flat upper surface 152, and has an opening 50 defined in the upper surface 152 thereof and a lid 52 for opening and closing the opening 50.
- FIG. 16 is a perspective view of each of fuel introducing members 160a, 160b of a fuel tank according to an eleventh embodiment of the present invention.
- Each of the fuel introducing members 160a, 160b is of a crescent shape (hollow three-dimensional shape) as viewed in front elevation which is curved upwardly (lower chord), and has an opening 50 defined in a curved upper surface 162 thereof and a lid 164 for opening and closing the opening 50.
- the lid 164 has a curved surface which corresponds to the curved upper surface 162.
- FIG. 17 is a perspective view of each of fuel introducing members 170a, 170b of a fuel tank according to a twelfth embodiment of the present invention.
- Each of the fuel introducing members 170a, 170b is of a crescent shape (hollow three-dimensional shape) as viewed in front elevation which is curved downwardly (upper chord), and has an opening 50 defined in a concave upper surface 172 thereof and a lid 174 for opening and closing the opening 50.
- the lid 174 has a concave surface which corresponds to the concave upper surface 172.
- the fifth through twelfth embodiments are set to various shapes, and essentially offer the same advantages as with the first through fourth embodiments.
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- General Engineering & Computer Science (AREA)
- Life Sciences & Earth Sciences (AREA)
- Sustainable Development (AREA)
- Sustainable Energy (AREA)
- Transportation (AREA)
- Cooling, Air Intake And Gas Exhaust, And Fuel Tank Arrangements In Propulsion Units (AREA)
Description
- The present invention relates to a fuel tank including a first reservoir for reserving fuel, a second reservoir for reserving the fuel, and a siphon tube which extends between the first reservoir and the second reservoir and which is evacuated by a negative pressure generator.
- Fuel tanks are used to supply fuel to internal combustion engines. For example, 4WD (four-wheel-drive) vehicles and FR (front engine, rear wheel drive) vehicles use a so-called saddle fuel tank, the bottom of which is upwardly recessed at the center portion in the width direction of the vehicle, in order for the fuel tank to avoid physical interference with the propeller shaft, which extends down the middle of the vehicle.
- The saddle fuel tank is generally divided into a first reservoir for reserving fuel and a second reservoir for reserving the fuel, and each of the first reservoir and the second reservoir is equipped with one fuel pumping system. Accordingly, the saddle fuel tank requires the two fuel pumping systems in comparison with fuel tanks for use in 2WD (two-wheel-drive) vehicles, and thus it is more costly and larger.
-
discloses a fuel tank including a first reservoir for storing fuel; a second reservoir for storing the fuel; and a siphon tube which extends between the first reservoir and the second reservoir and which is evacuated by a negative pressure generator; the fuel tank comprising a fuel introducing member connected to at least one open end of the siphon tube, wherein the fuel introducing member includes an opening for introducing the fuel therethrough; and a lid for closing the opening under its own weight of the lid when the liquid level of fuel has fallen just above the opening and the opening is disposed above the at least one open end of the siphon tube.JP 63 104671 U - In
DE 43 37 183 A1 , the open end of the siphon tube stands vertically, and this open end is closed by a lid which closes this opening under its own weight. -
DE 199 00 378 A1 discloses a saddle tank with a siphon tube connected to fuel introducing members equipped with a lid which opens and closes an inlet opening in dependence of a fuel level. -
discloses a fuel introducing member with an inlet opening oriented in an upward direction, closed by a lid moving in a downward direction.JP 64 028318 U - There is known a fuel tank level equalizer system as disclosed in Japanese Laid-Open Patent Publication No.
(hereinafter referred to as a "conventional art"). As shown in10-061515 FIG. 18 of the accompanying drawings, the fuel tank level equalizer system according to the conventional art includes afuel tank 1 having two 1a, 1b, and operates to equalize fuel levels in theseparate sections 1a, 1b through aseparate sections siphon 2. - The
separate section 1b houses therein afuel pump module 3 which has an outlet connected to a bypass pressure regulator 4. The regulator 4 has an outlet connected to aconduit 5 through which a liquid fuel is supplied to anozzle 6a of ajet pump 6. Thejet pump 6 is operated by the liquid fuel that is supplied to thenozzle 6a, drawing the fuel from 2a, 2b of thefuel pickups siphon 2 through thesiphon 2. - The fuel levels in the
1a, 1b are thus equalized through theseparate sections siphon 2, and a single fuel level sensor 7 can monitor all the fuel levels in the vehicle. - In the
above fuel tank 1, each of the 2a, 2b includes a flow valve assembly, not shown, which is actuated by a filter and a diaphragm. The filter is made of a flexible material having small openings, and the filter, when wetted, prevents air from flowing therethrough due to the capillary action of the liquid fuel. When there is no liquid fuel in the inlets of the fuel pickups, air is prevented from flowing therethrough by a liquid capillary seal of the filter.fuel pickups - However, the fuel tank level equalizer system according to the conventional art is made up of a number of components and is complex in structure because the system includes actuating parts such as the filter having the small openings, the diaphragm, etc., and also includes the flow valve assembly. Therefore, the fuel tank level equalizer system according to the conventional art is costly to manufacture, and is low in productivity and endurance reliability. Furthermore, the fuel undergoes a large pressure loss because it flows through the filter having the small openings, resulting in a reduced siphon transfer speed. Accordingly, the filter tends to be clogged with dirt and also tend to be damaged.
- In addition, since the fuel tank level equalizer system according to the conventional art has a liquid filter structure, the filter fails to provide a sealing function when it is dry, not wet. When the filter is dry, it does not prevent air from flowing therethrough, and thus the filter does not provide a stable siphon effect. For example, if the fuel is present in only the
separate section 1a, then no siphon effect is provided, and the fuel levels in the 1a, 1b can not be equalized.separate sections - The present invention has been made in an effort to solve the above problems. It is an object of the present invention to provide a fuel tank which is capable of providing a desired siphon effect and using fuel in the fuel tank efficiently with a simple and economic structure.
- According to the present invention, there is provided a fuel tank in accordance with
claim 1. The fuel tank includes a first reservoir for storing fuel, a second reservoir for storing the fuel, and a siphon tube which extends between the first reservoir and the second reservoir and which is evacuated by a negative pressure generator. - The fuel tank comprises a fuel introducing member connected to at least one open end of the siphon tube, wherein the fuel introducing member includes an opening for introducing the fuel therethrough, and a lid for closing the opening under its own weight of the lid when the opening is positioned above the liquid level of the fuel, and the opening is disposed below the at least one open end of the siphon tube.
- According to the present invention, the fuel introducing member, which is connected to at least one open end of the siphon tube, includes the opening for introducing the fuel in the fuel tank therethrough, and the opening is disposed below the upper end of the inner diameter of the one open end of the siphon tube. Therefore, the fuel can effectively be siphoned until the fuel level becomes lower than the upper end of the inner diameter of the at least one open end of the siphon tube. The fuel in the fuel tank can thus be used efficiently with a simple and economical structure.
-
-
FIG. 1 is a schematic structural view of a fuel tank according to a first embodiment of the present invention; -
FIG. 2 is a perspective view of a fuel introducing member in the fuel tank; -
FIG. 3 is a sectional side elevational view of the fuel introducing member; -
FIG. 4 is a front elevational view, partly in cross section, of the fuel introducing member; -
FIG. 5 is a view illustrative of operation of the fuel tank; -
FIG. 6 is a perspective view of each of fuel introducing members of a fuel tank according to a second embodiment of the present invention; -
FIG. 7 is a perspective view of each of fuel introducing members of a fuel tank according to a third embodiment of the present invention; -
FIG. 8 is a front elevational view of the fuel introducing member; -
FIG. 9 is a sectional side elevational view of each of fuel introducing members of a fuel tank according to a fourth embodiment of the present invention; -
FIG. 10 is a perspective view of each of fuel introducing members of a fuel tank according to a fifth embodiment of the present invention; -
FIG. 11 is a perspective view of each of fuel introducing members of a fuel tank according to a sixth embodiment of the present invention; -
FIG. 12 is a perspective view of each of fuel introducing members of a fuel tank according to a seventh embodiment of the present invention; -
FIG. 13 is a perspective view of each of fuel introducing members of a fuel tank according to an eighth embodiment of the present invention; -
FIG. 14 is a perspective view of each of fuel introducing members of a fuel tank according to a ninth embodiment of the present invention; -
FIG. 15 is a perspective view of each of fuel introducing members of a fuel tank according to a tenth embodiment of the present invention; -
FIG. 16 is a perspective view of each of fuel introducing members of a fuel tank according to an eleventh embodiment of the present invention; -
FIG. 17 is a perspective view of each of fuel introducing members of a fuel tank according to a twelfth embodiment of the present invention; and -
FIG. 18 is a view showing a fuel tank level equalizer system according to a conventional art. - As shown in
FIG. 1 , afuel tank 10 according to a first embodiment of the present invention comprises a saddle fuel tank, and is mounted on a vehicle, not shown. Thefuel tank 10 includes an upwardlycurved saddle 14 on its bottom substantially centrally in the width direction (indicated by the arrow A) of the vehicle. Thesaddle 14 defines a main tank (first reservoir) 16 and a sub-tank (second reservoir) 18 in thefuel tank 10. - A
fuel pump module 20 is disposed in themain tank 16. Thefuel pump module 20 comprises afuel pump 22 including apumping jet pump 24 which has afuel inlet port 24a that is open toward the bottom of aninner surface 16a of themain tank 16 and also including apressure regulator 26 connected to an outlet of thefuel pump 22. - The
pressure regulator 26 supplies a fuel F to an engine, not shown, through afuel pipe 28, and has asuction branch pipe 30 extending therefrom. Thebranch pipe 30 has a distal end (lower end) connected to asuction jet pump 32 as a negative pressure generator. - The
fuel tank 10 houses therein asiphon tube 34 extending over the bottoms of 16a, 18a of theinner surfaces main tank 16 and thesub-tank 18. Thesiphon tube 34 includes a three-way joint 36 in its upper portion which includes asuction connector 36a having acheck valve 38 disposed therein. Thesuction connector 36a is connected to an end of asuction tube 40, which has the other end connected to a suction side (negative pressure side) of thesuction jet pump 32. - The siphon
tube 34 has anopen end 34a disposed in themain tank 16 and directed in a width direction of the vehicle incorporating thefuel tank 10. Afuel introducing member 42a is connected to theopen end 34a. As shown inFIGS. 2 and3 , thefuel introducing member 42a is of a hollow three-dimensional shape, e.g., a hollow rectangular parallelepiped, which is short in height directions, i.e., in the directions indicated by the arrow B. Thefuel introducing member 42a basically comprises a base 44 in the form of a square tray and a substantiallyrectangular cover 46 mounted on thebase 44. - The
cover 46 includes a joint 48 which is formed integrally with thecover 46. To the joint 48, theopen end 34a of the siphontube 34 is connected. Thecover 46 has acircular opening 50 defined in anupper surface 46a thereof which is disposed below the upper end of an inner diameter of theopen end 34a of the siphon tube 34 (seeFIG. 3 ). - The
opening 50, which serves to introduce the fuel F from themain tank 16, is selectively opened and closed by alid 52. Thelid 52 is vertically openably and closably supported on theupper surface 46a of thecover 46 by apivot shaft 54. If necessary, a float (floating member) 55 may be mounted on thelid 52. When theopening 50 is positioned above the liquid level Fs of the fuel F, thelid 52 closes theopening 50 under its own weight. When theopening 50 is positioned below the liquid level Fs of the fuel F, thelid 52 floats in the fuel F, and then opens theopening 50. - If the
lid 52 itself has the above function, then thefloat 55 may be dispensed with. Thelid 52 has astopper 53 formed integrally therewith for regulating an open position (angular position for its swinging movement) of thelid 52. - The
upper surface 46a of thecover 46 has agroove 56 defined therein around theopening 50. Thebase 44 and thecover 46 define afuel channel 58 therebetween which connects theopening 50 and theopen end 34a of the siphontube 34 to each other. - As shown in
FIGS. 3 and4 , thefuel channel 58 has an opening area which is equal to or greater than the opening area of theopening 50. The opening area of theopening 50 and the opening area of thefuel channel 58 are equal to or greater than the opening area of theopen end 34a of the siphontube 34. - As shown in
FIG. 1 , the siphontube 34 has anopen end 34b disposed in the sub-tank 18. Afuel introducing member 42b is connected to theopen end 34b. Thefuel introducing member 42b is identical in structure to thefuel introducing member 42a. Those parts of thefuel introducing member 42b which are identical to those of thefuel introducing member 42a are denoted by identical reference characters, and will not be described below (seeFIGS. 2 through 4 ). At least one of the 42a, 42b may be employed.fuel introducing members - The
fuel pump module 20 includes afloat 60 for detecting the position of the liquid level Fs of the fuel F stored in themain tank 16. - Operation of the
fuel tank 10 will be described below. - When the
fuel pump 22 of thefuel pump module 20 is actuated, the fuel F stored in themain tank 16 is drawn from thefuel inlet port 24a by the pumpingjet pump 24. - The fuel F is supplied from the
pressure regulator 26 through thefuel pipe 28 to the engine, and is also supplied through thebranch pipe 30 to thesuction jet pump 32, developing a negative pressure in thesuction tube 40. Since thesuction tube 40 is connected to the siphontube 34 through the three-way joint 36, the siphontube 34 is evacuated. - The siphon
tube 34 has itsopen end 34a placed in the fuel F stored in themain tank 16 and its otheropen end 34b placed in the sub-tank 18 which is initially free of the fuel F, with thelid 52 of thefuel introducing member 42b being closed (seeFIG. 5 ). - When the siphon
tube 34 is evacuated by thesuction jet pump 32, the fuel F which has been drawn from theopen end 34a of the siphontube 34 through theopening 50 of thefuel introducing member 42a and thefuel channel 58 is delivered toward the otheropen end 34b of the siphontube 34. - When the
open end 34b of the siphontube 34 is supplied with the fuel F, thelid 52 of thefuel introducing member 42b is opened. The fuel F now flows from themain tank 16 into the sub-tank 18 due to the siphoning function of the siphontube 34. Therefore, the liquid level Fs of the fuel F in themain tank 16 and the liquid level Fs of the fuel F in the sub-tank 18 are brought into the same height. - According to the first embodiment, the
fuel introducing member 42a which is connected to theopen end 34a of the siphontube 34 is mounted on the bottom of themain tank 16, and has itsopening 50 disposed below the upper end of the inner diameter of theopen end 34a (seeFIG. 3 ). - Consequently, the fuel F can effectively be siphoned until the liquid level Fs becomes lower than the upper end of the inner diameter of the
open end 34a of the siphontube 34. The fuel F in themain tank 16 can thus be used efficiently with a simple and economical structure. - Furthermore, the
fuel introducing member 42a, which is mounted on the bottom of themain tank 16, is capable of effectively siphoning the fuel F stored in themain tank 16 without leaving a large quantity of fuel. - According to the first embodiment, in particular, the
fuel introducing member 42a is disposed in themain tank 16, and thefuel introducing member 42b is disposed in the sub-tank 18. Therefore, any remaining fuel F can efficiently be siphoned from both themain tank 16 and the sub-tank 18. - As shown in
FIG. 2 , each of the 42a, 42b is of a cubic or rectangular parallelepiped shape (hollow three-dimensional shape), which is short in a height direction, and has thefuel introducing members opening 50 defined in theupper surface 46a and thelid 52 for opening and closing theopening 50. Even in a case where the vehicle is tilted on a slope or the like, its own weight of thelid 52 prevents thelid 52 from swinging in a direction to open theopening 50. In addition, in the 42a, 42b, since thefuel introducing members lid 52 closes theopening 50, the opening area of theopening 50 can be set to a large size, thereby for protection of theopening 50 against clogging or the like. - Furthermore, the
groove 56 is defined in theupper surface 46a around theopening 50. When the remaining quantity of the fuel F is reduced and thelid 52 closes theopening 50 under its own weight, the fuel F remains around theopening 50 along thegroove 56. As a result, thelid 52 is brought into close contact with theupper surface 46a, and thus sealing performance of theopening 50 can be increased easily. - With the
42a, 42b, the opening area of thefuel introducing members fuel channel 58 is equal to or greater than the opening area of theopening 50. Therefore, no flow resistance is present on the passage from theopening 50 to thefuel channel 58, and thus the fuel F in themain tank 16 and the sub-tank 18 can smoothly flow from theopening 50 to thefuel channel 58. - Moreover, the opening area of the
opening 50 and the opening area of thefuel channel 58 are equal to or greater than the opening area of the open ends 34a, 34b of the siphontube 34. Consequently, the fuel F can smoothly and reliably flow through theopening 50 and thefuel channel 58 into the siphontube 34. -
FIG. 6 is a perspective view of each offuel introducing members 70a, 70b of a fuel tank according to a second embodiment of the present invention. - Those parts of the fuel tank according to the second embodiment which are identical to those of the
fuel tank 10 according to the first embodiment are denoted by identical reference characters, and will not be described below. Those parts of fuel tanks according to third and subsequent embodiments which are identical to those of thefuel tank 10 according to the first embodiment are also denoted by identical reference characters, and will not be described below. - The
upper surface 46a of thecover 46 of each of thefuel introducing members 70a, 70b has afirst region 72 including theopening 50 and asecond region 74 excluding theopening 50. Thefirst region 72 is at a level lower than thesecond region 74. - According to the second embodiment, when the remaining quantity of the fuel F is reduced and the
lid 52 closes theopening 50 under its own weight, since thefirst region 72 including theopening 50 is at a level lower than thesecond region 74, the fuel F tends to remain in thefirst region 72. Therefore, when thelid 52 closes theopening 50, the remaining fuel F performs a sealing function to cause thelid 52 to close theopening 50 reliably. -
FIG. 7 is a perspective view of each offuel introducing members 80a, 80b of a fuel tank according to a third embodiment of the present invention.FIG. 8 is a front elevational view of each of thefuel introducing members 80a, 80b. - Each of the
fuel introducing members 80a, 80b hasrecesses 82 defined at both sides of thelid 52, and a float (floating member) 84 is mounted on thelid 52. Thefloat 84 includesprojections 86 projecting downwardly into the respective recesses 82. Theprojections 86 have respective lower end faces 86a which are at a level lower than the opening 50 (seeFIG. 8 ). - According to the third embodiment, the lower end faces 86a which are positioned at the lower end of the
float 84 are at a level lower than theopening 50. Therefore, even in a case where the liquid level Fs of the fuel F is at a considerably low level, thefloat 84 exerts buoyant force thereby to open theopening 50. - Even when the liquid level Fs is lowered to a level that is close to the
opening 50 as much as possible, therefore, theopening 50 is reliably opened thereby to make it possible to draw in the fuel F. As a result, the fuel F that remains in the tank can thus be further reduced for easily achieving efficient use of the fuel F. -
FIG. 9 is a sectional side elevational view of each offuel introducing members 90a, 90b of a fuel tank according to a fourth embodiment of the present invention. - Each of the
fuel introducing members 90a, 90b includes a float (floating member) 94 mounted on thelid 52 by ajoint member 92. Thefloat 94 has a lower end positioned below theopening 50. - According to the fourth embodiment, the position where the
lid 52 is opened by thefloat 94 can be set as low as possible. Therefore, the fourth embodiment offers the same advantages as with the third embodiment, e.g., the fourth embodiment is efficient in that the remaining amount of the fuel F can be suitably reduced. -
FIG. 10 is a perspective view of each offuel introducing members 100a, 100b of a fuel tank according to a fifth embodiment of the present invention. - Each of the
fuel introducing members 100a, 100b is of an inverted trapezoidal shape (hollow three-dimensional shape) as viewed in front elevation with a narrower lower end, and includes anopening 50 defined in an upper surface thereof and alid 52 for opening and closing theopening 50. -
FIG. 11 is a perspective view of each offuel introducing members 110a, 110b of a fuel tank according to a sixth embodiment of the present invention. - Each of the
fuel introducing members 110a, 110b is of a hexagonal shape (hollow three-dimensional shape) as viewed in front elevation with widthwise opposite sides projecting outwardly in a dogleg shape, and includes anopening 50 defined in an upper surface thereof and alid 52 for opening and closing theopening 50. -
FIG. 12 is a perspective view of each offuel introducing members 120a, 120b of a fuel tank according to a seventh embodiment of the present invention. - Each of the
fuel introducing members 120a, 120b is of a trapezoidal shape (hollow three-dimensional shape) as viewed in front elevation with a wider lower end, and includes anopening 50 defined in an upper surface thereof and alid 52 for opening and closing theopening 50. -
FIG. 13 is a perspective view of each offuel introducing members 130a, 130b of a fuel tank according to an eighth embodiment of the present invention. - Each of the
fuel introducing members 130a, 130b is of an elliptical shape (hollow three-dimensional shape) as viewed in front elevation which is elongate transversely, and has anopening 50 defined in a curvedupper surface 132 thereof and alid 134 for opening and closing theopening 50. Thelid 134 has a curved surface which corresponds to the curvedupper surface 132. - Alternatively, each of the
fuel introducing members 130a, 130b may have a flat upper surface instead of the curvedupper surface 132, and also have anopening 50 defined in the flat upper surface thereof and alid 52 for opening and closing theopening 50. This holds true for ninth and subsequent embodiments to be described below. -
FIG. 14 is a perspective view of each offuel introducing members 140a, 140b of a fuel tank according to a ninth embodiment of the present invention. - Each of the
fuel introducing members 140a, 140b is of an upper semicircular shape (hollow three-dimensional shape) as viewed in front elevation with aflat bottom surface 142, and has anopening 50 defined in a curvedupper surface 144 thereof and alid 146 for opening and closing theopening 50. Thelid 146 has a curved surface which corresponds to the curvedupper surface 144. -
FIG. 15 is a perspective view of each offuel introducing members 150a, 150b of a fuel tank according to a tenth embodiment of the present invention. - Each of the
fuel introducing members 150a, 150b is of a lower semicircular shape (hollow three-dimensional shape) as viewed in front elevation with a flatupper surface 152, and has anopening 50 defined in theupper surface 152 thereof and alid 52 for opening and closing theopening 50. -
FIG. 16 is a perspective view of each offuel introducing members 160a, 160b of a fuel tank according to an eleventh embodiment of the present invention. - Each of the
fuel introducing members 160a, 160b is of a crescent shape (hollow three-dimensional shape) as viewed in front elevation which is curved upwardly (lower chord), and has anopening 50 defined in a curvedupper surface 162 thereof and alid 164 for opening and closing theopening 50. Thelid 164 has a curved surface which corresponds to the curvedupper surface 162. -
FIG. 17 is a perspective view of each offuel introducing members 170a, 170b of a fuel tank according to a twelfth embodiment of the present invention. - Each of the
fuel introducing members 170a, 170b is of a crescent shape (hollow three-dimensional shape) as viewed in front elevation which is curved downwardly (upper chord), and has anopening 50 defined in a concaveupper surface 172 thereof and alid 174 for opening and closing theopening 50. Thelid 174 has a concave surface which corresponds to the concaveupper surface 172. - The fifth through twelfth embodiments are set to various shapes, and essentially offer the same advantages as with the first through fourth embodiments.
Claims (10)
- A fuel tank including:a first reservoir (16) for storing fuel;a second reservoir (18) for storing the fuel;a siphon tube (34) which extends, with a first inner diameter, between the first reservoir (16) and the second reservoir (18), which is evacuated by a negative pressure generator, said siphon tube (34) having at least one open end (34a) disposed in one of the first reservoir (16) and the second reservoir (18);a fuel introducing member (42a) having a base (44) covered by a cover (46), wherein the cover (46) is integrally formed with a joint (48) connected to said at least one open end (34a) of the siphon tube (34), such that, at the joint (48), the siphon tube (34) has a second inner diameter larger than the first inner diameter;wherein an opening (50) is defined in the upper surface of the cover (46) for introducing the fuel therethrough; anda lid (52) for closing the opening (50) under its own weight of the lid (52) when the opening (50) is positioned above the liquid level (Fs) of the fuel, whereinthe fuel introducing member (42a) is of hollow three-dimensional shape which is shorter in a height direction than in the horizontal directions;wherein said at least one open end (34a) of the siphon tube (34) is oriented substantially parallel to a bottom surface of said one of the first reservoir (16) and the second reservoir (18); andwherein the opening (50) is disposed below the lower end of the first inner diameter of the siphon tube (34) at the joint (48).
- The fuel tank according to claim 1,
wherein the at least one open end (34a) of the siphon tube (34) adapted to be oriented in a width direction of a vehicle which incorporates the fuel tank. - The fuel tank according to claim 1,
wherein the opening (50) is open in an upward direction of the fuel tank, and the lid (52) closes the opening (50) in a downward direction of the fuel tank under its own weight of the lid (52) when the opening (50) is positioned above the liquid level of the fuel. - The fuel tank according to claim 1,
wherein the fuel introducing member (42a) is placed on a bottom of the first reservoir (16). - The fuel tank according to claim 1,
wherein the fuel introducing member comprises:a first fuel introducing member (42a) connected to the one open end (34a) of the siphon tube (34); anda second fuel introducing member (42b) connected to another open end (34b) of the siphon tube (34). - The fuel tank according to claim 1,
wherein the lid (52) includes a floating member (84) for exerting buoyant force to float the lid (52) in the fuel; and
the floating member (84) has a lower end which is positioned below the opening (50) when the lid (52) closes the opening (50). - The fuel tank according to claim 6, wherein the fuel introducing member (42a) has a groove (56) defined in the upper surface thereof around the opening (50).
- The fuel tank according to claim 6, wherein the upper surface of the fuel introducing member (70a) includes:a first region (72) including the opening (50); anda second region (74) excluding the opening (50);the first region (72) being at a level lower than the second region (74).
- The fuel tank according to claim 1,
wherein the fuel introducing member (42a) includes a fuel channel (58) for supplying the fuel introduced from the opening (50), to the at least one open end (34a) of the siphon tube (34); and
the fuel channel (58) has an opening area which is equal to or greater than the opening area of the opening (50). - The fuel tank according to claim 9,
wherein the opening area of the fuel channel (58) and the opening area of the opening (50) are equal to or greater than the opening area of the at least one open end (34a) of the siphon tube (34).
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP2009024992 | 2009-02-05 | ||
| PCT/JP2010/051382 WO2010090165A1 (en) | 2009-02-05 | 2010-02-02 | Fuel tank |
Publications (3)
| Publication Number | Publication Date |
|---|---|
| EP2394836A1 EP2394836A1 (en) | 2011-12-14 |
| EP2394836A4 EP2394836A4 (en) | 2012-10-10 |
| EP2394836B1 true EP2394836B1 (en) | 2015-08-19 |
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ID=42542059
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| EP10738497.6A Not-in-force EP2394836B1 (en) | 2009-02-05 | 2010-02-02 | Fuel tank |
Country Status (5)
| Country | Link |
|---|---|
| US (1) | US8944268B2 (en) |
| EP (1) | EP2394836B1 (en) |
| JP (1) | JP5497671B2 (en) |
| CN (1) | CN102300738B (en) |
| WO (1) | WO2010090165A1 (en) |
Families Citing this family (12)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102300738B (en) | 2009-02-05 | 2015-05-06 | 本田技研工业株式会社 | Fuel tank |
| WO2011007654A1 (en) * | 2009-07-16 | 2011-01-20 | 本田技研工業株式会社 | Fuel tank |
| JP5491366B2 (en) * | 2010-11-25 | 2014-05-14 | 本田技研工業株式会社 | Fuel supply device |
| EP2811145B1 (en) * | 2012-02-02 | 2017-06-14 | Toyota Jidosha Kabushiki Kaisha | Fuel supply device |
| EP2738032B1 (en) * | 2012-11-30 | 2016-02-03 | Magna Steyr Fuel Systems GesmbH | Tank system for a motor vehicle |
| US9486725B2 (en) * | 2013-02-21 | 2016-11-08 | Caterpillar Inc. | System and method for filtering fuel within fuel tank |
| US9470193B2 (en) * | 2013-03-22 | 2016-10-18 | Caterpillar Inc. | System and method for filtering fuel within fuel tank |
| JP5937764B2 (en) * | 2013-09-19 | 2016-06-22 | 本田技研工業株式会社 | Saddle-type vehicle and fuel strainer |
| WO2019122430A1 (en) * | 2017-12-22 | 2019-06-27 | Plastic Omnium Advanced Innovation And Research | Vehicle suction system |
| DE102018201117B3 (en) * | 2018-01-24 | 2019-07-04 | Ford Global Technologies, Llc | Assembly for a vehicle, in particular hybrid electric vehicle and vehicle, in particular hybrid electric vehicle |
| DE102018208643A1 (en) * | 2018-05-30 | 2019-12-05 | Röchling Automotive SE & Co. KG | Car tank assembly and removal module with a porous conveyor body |
| US10682908B1 (en) | 2019-01-07 | 2020-06-16 | Ford Global Technologies, Llc | Methods and systems for a fuel scavenge arrangement |
Family Cites Families (26)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2646061A (en) | 1947-08-19 | 1953-07-21 | Skuttle Mfg Company | Flush type humidifier |
| JPS63104671U (en) | 1986-12-25 | 1988-07-06 | ||
| JPH0511699Y2 (en) | 1987-08-12 | 1993-03-24 | ||
| DE3915185C1 (en) * | 1989-05-10 | 1990-10-04 | Daimler-Benz Aktiengesellschaft, 7000 Stuttgart, De | |
| US5170764A (en) | 1991-12-23 | 1992-12-15 | Walbro Corporation | Fuel pump pick-up system |
| US5363827A (en) | 1993-10-14 | 1994-11-15 | Carter Automotive Company, Inc. | Fuel pump assembly |
| DE4337183A1 (en) | 1993-10-30 | 1995-05-04 | Pierburg Gmbh | Device for the extraction of fuel |
| JPH07310598A (en) * | 1994-05-13 | 1995-11-28 | Honda Motor Co Ltd | Vaporizer float pivot structure |
| DE19547097A1 (en) * | 1995-12-16 | 1997-06-19 | Audi Ag | Device for supplying an internal combustion engine with fuel |
| US5979485A (en) * | 1996-07-01 | 1999-11-09 | Walbro Corporation | Fuel tank level equalizer system |
| US5724947A (en) | 1997-03-13 | 1998-03-10 | Om Corporation | Fuel pump unit |
| EP0979939B1 (en) * | 1998-08-10 | 2006-10-04 | Siemens Aktiengesellschaft | Fuel supply system |
| DE19900378B4 (en) * | 1999-01-08 | 2005-03-17 | Siemens Ag | tank system |
| JP2000356174A (en) * | 1999-06-11 | 2000-12-26 | Fuji Heavy Ind Ltd | Jet pump device |
| US6505644B2 (en) | 2000-06-09 | 2003-01-14 | Delphi Technologies, Inc. | Dual barrel jet fuel pump assembly for a fuel tank |
| DE10055355C2 (en) * | 2000-11-08 | 2003-07-10 | Kautex Textron Gmbh & Co Kg | Fuel tank |
| DE10154150A1 (en) * | 2001-11-03 | 2003-05-15 | Daimler Chrysler Ag | Fuel tank with venting system has line running from region of tank roof to low pressure region of suction jet pump |
| US6655403B2 (en) * | 2002-01-08 | 2003-12-02 | Eaton Corporation | Controlling fuel vapor venting in a fuel tank |
| JP2004232513A (en) * | 2003-01-29 | 2004-08-19 | Hitachi Unisia Automotive Ltd | Fuel supply system and fuel transfer tube for internal combustion engine |
| US6871640B2 (en) * | 2003-03-18 | 2005-03-29 | Ti Group Automotive Systems, Inc. | Saddle tank siphon primer |
| DE10342081B4 (en) * | 2003-09-10 | 2006-08-10 | Siemens Ag | Fuel tank for a motor vehicle |
| US7069913B1 (en) | 2005-08-18 | 2006-07-04 | Ti Group Automotive Systems, L.L.C. | Fuel delivery system for a combustion engine |
| US7284540B2 (en) * | 2006-03-16 | 2007-10-23 | Denso International America, Inc. | Fuel pump module anti-siphon valve |
| DE102006059967A1 (en) | 2006-12-19 | 2008-06-26 | GM Global Technology Operations, Inc., Detroit | Suction-pipe venturi nozzle for motor vehicle saddle fuel tank, has float valve arranged inside suction pipe |
| JP4980936B2 (en) * | 2008-01-10 | 2012-07-18 | トヨタ自動車株式会社 | Fuel tank structure |
| CN102300738B (en) | 2009-02-05 | 2015-05-06 | 本田技研工业株式会社 | Fuel tank |
-
2010
- 2010-02-02 CN CN201080006146.7A patent/CN102300738B/en not_active Expired - Fee Related
- 2010-02-02 US US13/147,223 patent/US8944268B2/en not_active Expired - Fee Related
- 2010-02-02 EP EP10738497.6A patent/EP2394836B1/en not_active Not-in-force
- 2010-02-02 WO PCT/JP2010/051382 patent/WO2010090165A1/en not_active Ceased
- 2010-02-02 JP JP2010549461A patent/JP5497671B2/en not_active Expired - Fee Related
Also Published As
| Publication number | Publication date |
|---|---|
| EP2394836A4 (en) | 2012-10-10 |
| US20110290793A1 (en) | 2011-12-01 |
| JPWO2010090165A1 (en) | 2012-08-09 |
| WO2010090165A1 (en) | 2010-08-12 |
| US8944268B2 (en) | 2015-02-03 |
| EP2394836A1 (en) | 2011-12-14 |
| CN102300738B (en) | 2015-05-06 |
| CN102300738A (en) | 2011-12-28 |
| JP5497671B2 (en) | 2014-05-21 |
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